Influence of bolt spacing and degree of anisotropy in single-lap joints

Computers and Structures

Volumn 76, Issue 1, 2000, Pages 89-103

  Sergeev, B ^a   Madenci, E ^a   Ambur, D R ^b  

^a University of Arizona   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANISOTROPY; BOUNDARY CONDITIONS; COMPOSITE STRUCTURES; FAILURE ANALYSIS; GEOMETRY; STRESSES;

BOLT LOAD DISTRIBUTION; BOLT SPACING; BOUNDARY COLLOCATION TECHNIQUE; CONTACT STRESS;

BOLTED JOINTS;

EID: 0033889868     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0045-7949(99)00142-X     Document Type: Article

References (4)

1. Ramkumar RL, Seather ES, Appa K. Stress analysis of laminated and metallic plates bolted together by many fasteners, Final Report AFWAL-TR-86-3034, Aircraft Division, Northrop Corporation, El Segundo, CA, 1986.
2. Lekhnitskii S.G. Anisotropic Plates. 1968;Gordon & Breach, New York.
3. Bowie O.L., Neal D.M. A modified mapping collocation technique for accurate calculation of stress intensity factors. International Journal of Fracture Mechanics. 6:1970;199-206.
4. Sergeev BA. Analysis of composite laminates with multiple fasteners by boundary collocation technique. Ph.D. thesis, University of Arizona, Tucson, 1997.